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Systems Day 1 Flashcards

1
Q

Model of Power Plant

A

PW150A

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2
Q

Normal Takeoff Power?

A

4580 SHP

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3
Q

Max takeoff Power? (MTOP)

A

5071 SHP

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4
Q

MRW

A

29,089 kg

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5
Q

MTOW

A

28,998 kg

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6
Q

MLW

A

28,009 kg

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7
Q

MZFW

A

25,855 kg

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8
Q

Altitude alerts?

A

Passing within 1000 ft of selected
Deviations greater than 250 ft

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9
Q

Overspeed warnings

A

Steady beeping tone. Airspeed display turns red. -2kts below for it to deactivate

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10
Q

How many AOA vanes for stick shaker?

A

1

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11
Q

SPS inhibited?

A

When airspeed is below 215kts and altitude is above 200ft RA

Stick pusher inhibited below 200ft

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12
Q

When will trend arrow show on TCAS?

A

When rate of change is above 500fpm

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13
Q

When is 2nm range ring displayed on TCAS?

A

During continuous mode and during TA and RA 10nn auto range.

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14
Q

What is default mode on TCAS?

A

Pop up mode

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15
Q

What does above mode monitor on TCAS?

A

9000ft above, 2700 feet below

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16
Q

Cyan Diamonds on TCAS?

A

Hollow - other traffic
Solid proximity intruder traffic (less thank 1200ft or 6nm)

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17
Q

RA display on TCAS?

A

Solid red square

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18
Q

RA inhibited?

A

Below 1100ft on climb
Below 900ft on descent

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19
Q

TCAS inhibits increase descent?

A

Below 1450 ft AGL (RA)

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20
Q

When are TCAS aural advisories inhibited?

A

Below 600ft on climb
Below 400ft on descent

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21
Q

When are climb RAs inhibited?

A

During engine out conditions.

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22
Q

When is increase climb RA inhibited?

A

In takeoff configuration (auto feather armed)
In landing configuration (when gear is down and flaps 15 or more)

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23
Q

What screens and controls operate in ESS bus?

A

MFD1 and ED
All push buttons and MFD1 rev button

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24
Q

Will ED Revert automatically?

A

Yes, is automatic 1 sec after failure if airspeed is greater than 50kts

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25
Which ICP and heading/course controls are linked?
Speed bugs are connected DH and MDA are not linked CDI are not linked HDG - linked
26
When does IAS mismatch display?
When there is a 10kt difference. Caution illuminates at 17kts
27
What message displays during manual ADC selection?
Yellow ADC1(2) on both PFDs
28
How long does AHRS alignment take?
60 seconds on ground 90 seconds in flight
29
PITCH/ROLL MISMATCH
When pitch or roll differs by 3 degrees. Pitch has priority.
30
Indication when using AHRS manual selection?
Yellow ATT1(2)/HDG1(2) display on PFD and ED
31
What happens to AHRS without TAS?
Reverts to basic attitude mode. In this mode the associated EADI operates like conventional mechanical AH. Basic light illuminates as only indication of being in this mode.
32
What is Directional Gyro DG mode?
Selected after failure of flux calve or magnetic detector unit. DG is selected and red slave illuminates. DG slew can be used for small corrections.
33
Indication of Heading Mismatch?
HDG MISMATCH on FMA. Yellow HDG flag on both PFDs. Difference of 8 degrees or more.
34
Radio altitude Mismatch?
Displays RAD ALT MISMATCH in yellow on FMA. Continues to display RA in yellow
35
Radio Altimeter failure?
If one fails continues to display other one. If both fail replaced by white dashes.
36
When is avionics fan inhibited?
Below 5 degrees on ground
37
What fans operate on battery?
Fan 1 will operate at 50% (fan2 backup)
38
How many avionics fans need to fail for caution?
2 fans and plane on ground.
39
Default Nav source on pilots side?
VOR/ILS1 (cyan)
40
What causes Nav source to turn yellow on PFD?
Offside selection or same selection as other side
41
Excess deviation occurs?
Dual FD ILS outside 1 dot Below 1200ft RA (LOC EXCESS and CDI flashes yellow)
42
Glide slope vs fms display?
Glideslope blue “G” FMS VNAV Magenta “V”
43
Glideslope Mismatch?
Discrepancy between nav receiver output not freq selection
44
GS EXCESS DEV
If GS goes off scale below 1200 ft AGL
45
How to override forced standby on radar?
4 pushes of Stab in 3 second
46
What axis is stabilisation given to Radar?
Pitch and Roll
47
How long does WAIT display on MFD for radar?
40-100 seconds
48
How many FGMs required for FD?
1
49
AP min altitudes?
1000ft on takeoff 200ft on landing 1000ft engine out
50
AP Manual disengagement?
AP Disengage switch Deselecting AP Selecting GA button Manual pitch trim selection
51
CVR recording duration
2 hrs
52
FDR recording duration
25 hours
53
ELT Powered by
Internal battery
54
DC Starter converts to Generator at what point?
50%
55
How is DC Generator cooled?
Air cooled
56
Three DC battery voltage and load?
24V 40 Ah
57
Fuel Capacity
5318 kg
58
Maximum fuel imbalance
272kg
59
DC GEN output
28.5 volts 400 amps
60
What systems run off AC
AUX Fuel pump Standby Hydraulic pump TRUS De ice system (not stby pitot)
61
AC electrical power provided by generators when?
400 Np 850RPM
62
Power output of TRUS?
28V 300amp
63
Hot battery bus
Clocks 1&2 Batt master switch Battery power for refueling Fire bottle discharge squibs Fuel and hyd shutoff valves Engine FMUs Cargo fire suppression APU fire bottle squib manual discharge Flight deck dome lights and boarding lights Emergency PA system (10 total)
64
Battery limitations takeoff
-20 degrees. 0.1 load
65
ENG FUEL PRESS light means what?
Engine driven pump inlet pressure low
66
Hydraulic Reservoir quantity?
#1, #2 40% #3 45%
67
Nominal hydraulic pressure?
#1,2 3000PSI #3 2600-3250 PSI
68
Pressure required in #1 hyd system to power PTU?
2400 PSI more than 0 fluid
69
#1 hydraulic system users?
B rakes F laps A ntiskid I nboard spoiler R udder lower P TU E legatos outer BAI cut off by isolation valve
70
Hydraulic System #2 users?
L anding gear O utbord roll spoiler N osewheel steering E mergency park brake R udder upper E levator centre LONE cut off by isolation valve
71
Hydraulic number 3 users?
Elevator Inboard
72
Hydraulic isolation valve vs priority?
Isolation - low fluid quantity Priority - low pressure
73
#3 HYD pump?
Low pressure (900PSI) DCMP pump running for more than 60 sec on ground with eng running

Q400 Systems (8 decks)

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